TY - GEN
T1 - 3D inverse method for turbomachine blading with splitter blades
AU - Qiu, X.
AU - Dang, T.
N1 - Publisher Copyright:
Copyright © 2000 by ASME.
PY - 2000
Y1 - 2000
N2 - The use of a full 3D and viscous inverse method for turbomachine blading with splitter blades is demonstrated by carrying out a design modification of a transonic axial stator blade row with splitter blades. In this design modification study, the goal is to improve the aerodynamics of the full blade and the splitter blade, including weakening of shock wave and control of flow incidence. The improved blade design is "validated" using a well-known 3D Navier-Stokes analysis solver.
AB - The use of a full 3D and viscous inverse method for turbomachine blading with splitter blades is demonstrated by carrying out a design modification of a transonic axial stator blade row with splitter blades. In this design modification study, the goal is to improve the aerodynamics of the full blade and the splitter blade, including weakening of shock wave and control of flow incidence. The improved blade design is "validated" using a well-known 3D Navier-Stokes analysis solver.
UR - http://www.scopus.com/inward/record.url?scp=84955075292&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84955075292&partnerID=8YFLogxK
U2 - 10.1115/2000-GT-0526
DO - 10.1115/2000-GT-0526
M3 - Conference contribution
AN - SCOPUS:84955075292
T3 - Proceedings of the ASME Turbo Expo
BT - Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000
Y2 - 8 May 2000 through 11 May 2000
ER -